NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Sub-Scale Orion Parachute Test Results from the National Full-Scale Aerodynamics Complex 80- By 120-ft Wind TunnelA two-week test campaign was conducted in the National Full-Scale Aerodynamics Complex 80 x 120-ft Wind Tunnel in support of Orion parachute pendulum mitigation activities. The test gathered static aerodynamic data using an instrumented, 3-tether system attached to the parachute vent in combination with an instrumented parachute riser. Dynamic data was also gathered by releasing the tether system and measuring canopy performance using photogrammetry. Several canopy configurations were tested and compared against the current Orion parachute design to understand changes in drag performance and aerodynamic stability. These configurations included canopies with varying levels and locations of geometric porosity as well as sails with increased levels of fullness. In total, 37 runs were completed for a total of 392 data points. Immediately after the end of the testing campaign a down-select decision was made based on preliminary data to support follow-on sub-scale air drop testing. A summary of a more rigorous analysis of the test data is also presented.
Document ID
20170004354
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Anderson, Brian P.
(NASA Johnson Space Center Houston, TX, United States)
Greathouse, James S.
(NASA Johnson Space Center Houston, TX, United States)
Powell, Jessica M.
(NASA Johnson Space Center Houston, TX, United States)
Ross, James C.
(NASA Ames Research Center Moffett Field, CA, United States)
Schairer, Edward T.
(NASA Ames Research Center Moffett Field, CA, United States)
Kushner, Laura
(NASA Ames Research Center Moffett Field, CA, United States)
Porter, Barry J.
(NASA Ames Research Center Moffett Field, CA, United States)
Goulding, Patrick W., II
(Aerospace Solutions, LLC Moffett Field, CA, United States)
Zwicker, Matthew L.
(Airborne Systems North America Santa Ana, CA, United States)
Mollmann, Catherine
(Jacobs Technology, Inc. Houston, TX, United States)
Date Acquired
May 3, 2017
Publication Date
June 5, 2017
Subject Category
Aerodynamics
Report/Patent Number
JSC-CN-39271
Meeting Information
Meeting: AIAA Aerodynamics Decelerator Systems Technology Conference
Location: Denver, CO
Country: United States
Start Date: June 5, 2017
End Date: June 9, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 747797.06.14.03.99.10
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available